View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 00107U 26040.19552528 +.00000000 +00000-0 +72208-3 0 00002
2 00107 28.7790 334.1461 0495732 13.2789 348.0328 14.21454732 06
| Epoch (UTC): | 09 February 2026 04:41:33 |
| Eccentricity: | 0.0495732 |
| inclination: | 28.7790° |
| perigee height: | 464 km |
| apogee height: | 1177 km |
| right ascension of ascending node: | 334.1461° |
| argument of perigee: | 13.2789° |
| revolutions per day: | 14.21454732 |
| mean anomaly at epoch: | 348.0328° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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